Gotha Go 146

From Wikipedia, the free encyclopedia

Go 146
Type Utility aircraft
National origin Germany
Manufacturer Gotha
Designed by Albert Kalkert
Maiden flight 1936
Number built ca. 4

The Gotha Go 146 was a twin-engine utility aircraft developed in Germany in the mid-1930s. It was a conventional low-wing cantilever monoplane with tailwheel undercarriage, the main units of which retracted into the engine nacelles on the wings. It was offered to the Luftwaffe as a high-speed courier aircraft, but the Siebel Fh 104 was selected instead. With Gotha unable to attract other customers, no serious production was undertaken and a small number of prototypes were the only examples built.

[edit] Specifications

General characteristics

  • Crew: One pilot
  • Capacity: 4 passengers
  • Length: 9.45 m (31 ft 0 in)
  • Wingspan: 12.40 m (40 ft 8 in)
  • Height: 2.70 m (8 ft 10 in)
  • Wing area: 21.7 m² (234 ft²)
  • Empty weight: 1,520 kg (3,350 lb)
  • Gross weight: 2,200 kg (4,850 lb)
  • Powerplant: 2 × Hirth HM 508E, 180 kW (240 hp) each

Performance

  • Maximum speed: 335 km/h (208 mph)
  • Range: 1,000 km (620 miles)
  • Service ceiling: 5,000 m (16,400 ft)
  • Rate of climb: 7.5 m/s (1,470 ft/min)

[edit] References

  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions, 427. 
  • Nowarra, Heinz (1983). Die deutsche Luftrüstung 1933-1945. Bonn: Bernard and Graefe, Teil 2, p.133-34. 
  • "At the Brussels Show" (3 June 1937). Flight: 556. 
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Aircraft produced by Gothaer Waggonfabrik

Company designations pre-1918
LD.1 • LD.2 • LD.3 • LD.4 • LD.5 • LD.6 • LD.7

LE.1 • LE.2 • LE.3

WD.1 • WD.2 • WD.3 • WD.4 • WD.5 • WD.7 • WD.8 • WD.9 • WD.11 • WD.12 • WD.13 • WD.14 • WD.15 • WD.20 • WD.22 • WD.27


Idflieg designations 1914-1918
G.I • G.II • G.III • G.IV • G.V • G.VI • G.VII • G.VIII • G.IX • G.X


Reichsluftfahrtministerium designations 1933-1945
Go 145 • Go 146 • Go 147 • Go 149 • Go 150 • Go 229 • Go 241 • Go 242 • Go 244 • Go 345 • Ka 430
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